Pressurized panel

ABSTRACT

Large area pressurized meteoroid penetration detector panels. The structure of the panels includes an interconnected cellular configuration in which the cells have spaced periphery welds and tufts in their centers at which point a spot-weld is made joining the panels.

United States Patent 1 91 1111 3,744,320 White July 10, 1973 PRESSURIZED PANEL [56] References Cited [75] Inventor: Erskine C. White, Newport News, UNITED STATES PATENTS 3,526,139 9/1970 Mayo et a]. 73/432 R 3,238,774 3/1966 Gurtler 73/170 R [73] Assgnee' The U'med Amen as 3,446,068 5/1969 Slattery et al 73/170 R 22 Filed: Nov. 6, i970 Attorney-Howard J. Osborn [21] Appl. No.2 97,472 57 ABSTRACT Related Application Dam Large area pressurized meteoroid penetration detector [62], Division of I968 panels. The structure of the panels includes an interconnected cellular configuration in which the cells 2% 5"- 73/432 ag have spaced periphery welds and tufts in their centers E g 2 R i 6 R at which point a spot-weld is made joining the panels.

1 5 Claims, 2 Drawing Figures V: \s 11 41 4o represented by the Administrator of the National Aeronautics and Space Administration, Washington, DC.

Primary Examiner-Charles A. Ruehl Assistant Examiner-Joseph W. Roskos Patented July 10, 1973 3,744,320

FIG. 2

INVENTOR ATTORNEY ERSKINE C. WHITE PRESSURIZED PANEL This application is a division of application Ser. No. 777,765 filed Nov. 21, 1968.

The invention herein described was made to easily provide relatively flat, large area pressurized meteoroid penetration detectors having maximum inherent structural rigidity. These panels measure directly the penetration rate in materials to be used in spacecraft. Previous detectors were semicylindrical pressurized cell detectors with small penetration areas which measured penetration rates in very thin materials. These were relatively heavy configurations, often weighing 1.6 pounds per foot of penetration area. Furthermore, the design and small size of each sensor pennitted the presentation of only one penetration area (0.1 sq. ft. per sensor), while the method of fabrication, hand soldering, proved to be extremely tedious, time-consuming, and costly. In addition, the soldering method is not compatible with the high temperature environments of many planned missions. The present invention overcomes these shortcomings by providing unique metal forming fabrication techniques to readily produce a new type of pressure panel that has a maximum penetration sensitive area-to-weight ratio, i.e., of at least 0.787 lbs. per foot of penetration area, as well as low volume. Other advantages are minimum area lost due to fabrication, the ability to obtain various sizes and shapes, and simplicity of forming and fabricating panels having inherent structural rigidity without preforming the material.

It is therefore an object of this invention to provide a pressure panel that has a maximum penetration areato-weight ratio, low volume, and inherent structural rigidity.

Yet another object of the invention is to provide a micrometeoroid detection panel which has both sides exposed to meteoroid penetration.

Still another object of the invention is to provide a micrometeoroid detection panel capable of being used in the temperature environments of various planets.

An additional object of the invention is to provide a micrometeoroid detector panel which can be constructed of various thicknesses enabling penetration testing of a variety of sizes and velocities of meteoroids.

Another object of the invention is to provide an apparatus and a method for the easy production of detector panels having the hereinbefore mentioned advan tages.

These and other advantages of the present invention will become more readily apparent from the following description.

In the drawings:

FIG. I is an isometric view of a finished meteoroid detector panel having centrally tufted cells in a hexagonal configuration.

FIG. 2 is an exploded isometric view of the apparatus for the-pressure forming fabrication of the detector panels of the present invention including an unfinished panel.

Referring to the drawing in detail, FIG. 1 shows a completed pressure formed pressurized detector panel designated generally by the numeral 10. The detector panel has hexagonally shaped cells 11, a welded perimeter seam l4 and spaced cell perimeter welds 16 which create vent spaces 19 between the cells 11. The cells 11 have tufted centers 17 at which point a spot weld has been made. The tufted center-spot weld configuration has been found to greatly increase the overall structural rigidity of the panel. The detector panel 10 can be made to have cells conforming to any geometric shape. However, it has been found that the hexagonal configuration provides the greatest panel rigidity because there are no straight line elements to permit bending.

FIG. 2- shows an explided isometric view of the apparatus for pressure forming the detector panels 10. A prewelded panel, i.e., is formed by placing two cleaned sheets 12 and 13 of the metal desired to be tested together and welding the panel perimeter seams 14, the cell center spot wels 15, and the space cell perimeter seams 16, the panel is then placed between two plates of pressure forming apparatus. These consist of metal bases 24 and 25 upon which steel perimeter clamping plates 20 and 21 are screw mounted. The inner borders of these plates conform to the shape and size of the panel perimeter seam 14. Located beneath these are surface restricting shims 22 and 23. These shims have linear surface protrusions 27 which regulate the expan sion of the sheets at the vent spaces, and circular protrusions 26 which regulate expansion at the center spot welds. The shims serve a purpose more fully explained hereinafter.

The prewelded panel has a compressed air hose fitting 18 attached by means of copper tubing to one sheet in one corner of the panel. There is an aperture 32 in the upper half of the pressure forming apparatus through which this fitting 18 protrudes so that once the panel sheets are properly clamped in the pressure forming apparatus, the compressed air hose may be attached and the proper pressure of compressed air applied to the panel.

Two positioning pins 27 and 29 which are attached to the steel perimeter clamping plate 20, fit into two apertures 30 and 31 located in the steel perimeter clamping plate 21. These pins serve to properly aline the apparatus parts.

The prewelded panel plate is placed in position on top of the perimeter clamping plate 20 and overlapping edges are crimped down along the sides of the metal base 24. Holes 35 are bored in the sheets so that steel clamping bands 34 may be tightly bolted to the sides of the metal base 24 by bolts 33 screwed into threaded bores 36 located in the sides of the metal base 20. In this way the crimped-over panel sheets are securely fastened between the bands 34 and the sides of the base 24. This is done to prevent the panel sheet from pulling in in response to stresses exerted upon it during the pressure forming process, for it has been found that the panel has a tendency to pull in after a certain amount of deformation has taken place when air pressure is introduced between the sheets 12 and 13. This is especially true depending on the thickness of the panels.

Once the panel has been adequately'secured so as to I 3 corners to be expanded to the desired shape. After this initial pressure forming procedure is completed, the air pressure is released and the restrictions removed.

The now partially formed panel is then clamped between a second set of shims to limit the panel cell thickness to 0.250 inch. The panel is then pressurized to 100 pounds per square inch to expand the cells about their peripheries to the 0.250 inch thickness. Air pressure is then released and all surface restricting shims removed.

While still in the perimeter clamping device, the panel is then pressurized to 65 pounds per square inch, completing the cell formation. After depressurization, the formed panel is removed from the clamping device. A pressure sensor of the type disclosed in US. Pat. No. 3,238,774 is attached to one of the cells. For purposes of illustration, such a pressure sensor is shown diagrammatically in FIG. 1 and is designated by the reference numeral 40. Lines 41 connect the sensor with one of the cells. Final pressurization to 45 pounds per square inch is accomplished at table top at which time the copper tube of the fitting 18 is crimped together, the fitting removed, and the remaining length of tubing coiled up. The panel is now ready to be incorporated into its satellite configuration.

Because the cells are interconnected, the penetration of any one of them by a meteoroid results in a pressure .drop in the entire panel. The pressure sensor detects been described, it will be understood that modifications and improvements may be made thereto. Such of these modifications and improvements as incorporate the principles of this invention may be considered as included in the hereafter appended claims unless these claims by their language expressly state otherwise.

What is claimed as new and desired to be secured by Letters Patent is:

1. An apparatus for detecting meteoroid penetration comprising:

a large area detector panel means having a plurality of interconnected pressurized cells pressure formed therein, said panel means including at least a pair of opposed panels being sealed around their periphery and said cells being tufted in their centers at which point a junction is made between said opposed panels so as to give greater structural stability to the entire panel means while facilitating reduced internal volume; and

means for detecting and permanently recording pressure drop in said cells due to meteoroid penetration of said panel.

2. The apparatus as in claim 1 in which the cells are hexagonal in shape, said hexagonal configuration having more inherent structural rigidity. v

3. The apparatus as in claim 1 wherein the cell perimeters are welded; and spaces in said perimeter welds to provide means for communication between the cells.

4. The apparatus as in claim 1 in which the cells can be formed in any desired configuration.

5. The apparatus as in claim 1 wherein said tufted junction is a spot-weld. 

1. An apparatus for detecting meteoroid penetration comprising: a large area detector panel means having a plurality of interconnected pressurized cells pressure formed therein, said panel means including at least a pair of opposed panels being sealed around their periphery and said cells being tufted in their centers at which point a junction is made between said opposed panels so as to give greater structural stability to the entire panel means while facilitating reduced internal volume; and means for detecting and permanently recording pressure drop in said cells due to meteoroid penetration of said panel.
 2. The apparatus as in claim 1 in which the cells are hexagonal in shape, said hexagonal configuration having more inherent structural rigidity.
 3. The apparatus as in claim 1 wherein the cell perimeters are welded; and spaces in said perimeter welds to provide means for communication between the cells.
 4. The apparatus as in claim 1 in which the cells can be formed in any desired configuration.
 5. The apparatus as in claim 1 wherein said tufted junction is a spot-weld. 